STRUCTURE AND PROPERTIES OF THE WORKING BLADES OF AIRCRAFT GAS TURBINE ENGINES MADE OF HEAT-RESISTANT NICKEL ALLOY ZhS32-VI. plit-periodical [Internet]. 2026 Sep. 7 [cited 2026 Oct. 23];165(3):34-47. Available from: https://plit-periodical.org.ua/index.php/plit/article/view/328